N216WR
Service difficulty reports · 301
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N216WR' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N216WR' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2023031601769Floor Panel · peelingAFT CABIN FLOOR PANEL 242TF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 242 TF; P/N 147A5810-94; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS728;[02] VERIFIED STEP 1 RECEIVING FLOOR PANEL 242TF AND TO BE INSTALLED ON TTG8Q00GS728SDR SWAA2023031601768Floor Panel · peelingAFT CABIN FLOOR PANEL 242RF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 242 RF; P/N147A5810-2; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS72C;[02] VERIFIED STEP 1.SDR SWAA2023032001756Vapor Barrier · crackedRT BS 663 VAPOR BARRIER CRACK AT RBL 48<[01] PREPARED DAMAGED AREA FOR REPAIR; AND PERFORMED DRY OUT; FOUND NO WATER; AS PER B737 SRM 51-70-04-2R-10.;[02] VERIFIED STEP 1; OK TO INSTALL REPAIR.;[03] APPLIED REPAIR AT R\H ON VAPOR BARRIER PER B737SRM 51-70-04-2SDR SWAA2023031601453Floor Panel · delaminatedCABIN FLOOR PANEL 232BF FWD SIDE DELAMINATED<[01] PREPARED FOR REPAIR CABIN FLOOR PANEL 232 BF; AS PER B 737 SRM 53-00-50-2R-9.;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED FLOOR PANEL 232BF; AS PER B737; SRM 53-00-50-2R-9 MATERIAL USED PO.1473813 ASDR SWAA2023031601449Floor Panel · delaminatedCABIN FLOOR PANEL 231BF SURFACE DELAMINATED<[01] RECEIVED NEW CABIN FLOOR PANEL 231 BF; P/N 141A5810-168; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GXTW0;[02] VERIFIED STEP 1.SDR SWAA2023032000764Support Angle · crackedCENTER WING REAR SPAR VAPOR WEB RIGHT SIDE FRONT WALL ACCESS BY AC BAY SUPPORT ANGLE SIGNS OF CRACK DOR EV16<[01] PERFORMED HFEC ON UPPER SUPPORT ANGLE PER B737 NDT PART 6 51-00-00 PROC.23; SUPPORT HAS APROX. 0.625' CRACK. TOOL USED OLYMPUS NORTEC 600; B/C 166SDR SWAA2023032000773Floor Panel · delaminatedCABIN FLOOR PANEL 241FF FWD CORNER DELAMINATED<[01] PREPARED FOR REPAIR FLOOR PANEL 241 FF; AS PER B737 SRM 53-00-50-2R-9.;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED FLOOR PANEL 241 FF; AS PER B737; SRM 53-00-50-2R-9 MATERIAL USED PO.1473815 AND PSDR SWAA2023032000774Floor Panel · delaminatedCABIN FLOOR PANEL 242DF DELAMINATED<[01] MEASUREMENTS;[02] PREPARED DAMAGED AREA TO APPLY REPAIR AT FLOOR PANEL #242DF PER B737<BR>SRM 53-00-50-2R-7;[03] VERIFIED STEPS 1 AND 2;[04] OK TO APPLY REPAIR;[05] APPLIED REPAIR AT FLOOR PANEL #242DF PER B737<BR>SRM 5SDR SWAA2023032000354Panel · crackedLH UNDERWING ACCESS PANEL 192HL LOWER SURFACE AROUND FASTENER HOLE HAS MATERIAL CRACKED.<[01] PREPARED FOR REPAIR PANEL 192HL; AS PER B737 SRM 51-70-06-2R-9;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED PANEL 192HL; AS PER B737 SRM 51-70-06-2R-9 MATESDR SWAA2023031600775Floor Panel · delaminatedCABIN FLOOR PANEL 231FF L/H AREA DELAMINATED FLOOR PANEL 231 FF<[01] PREPARED FOR REPAIR; FLOOR PANEL 221 FF; AS PER B737 SRM 53-00-50-2R-9;[02] CORRECTION #1. PREPARED FOR REPAIR FLOOR PANEL 231FF; AS PER B737 SRM 53-00-50-2R-9;[03] VERIFIED CORRECTED STEP 2.SDR SWAA2023031601118Angle · crackedCENTER WING VAPOR WEB FWD WALL AREA ABOUT RBL10 SUPPORT ANGLE EVIDENCE OF CRACK<[01] PERFORMED A HFEC INSP. ON SUPPORT ANGLE PER B737 NDT PART 6 51-00-00 PROC. 23; 0.500' CRACK CONFIRMED. TOOL USED OLYMPUS NORTEC 600; B/C 172389; CAL DUE DATE 03/23.;[23] REMOVSDR SWAA2023031600770Girt Bar · out of adjustR1 DOOR SLIDE GIRT NEEDS REPACK<[01] NON-ROUTINE WRITTEN IN ERROR. SHOULD READ R1 DOOR SLIDE SKIRT IS TOUCHING CABIN FLOOR. [TTG8Q00J0H2Y];[02] VERIFIED STEP 1SDR SWAA2023032000353Panel · elongatedACCESS PANEL 661BB SEVERAL HOLES ENLONGATED<[01] PREPARED AREA FOR REAPAIR HOLES AT PANEL#661BB AS PER B737 SRM 51-70-04-2R-9;[02] REPAIRED DAMAGED AREA AT PANEL#661BB AS PER B737 SRM 51-70-04-2R-9 MATERIAL USED PO#1690463 PO#1800112;[03] VERIFIED STEPS 1 AND SDR SWAA2022092283064Slide · out of positionFWD ENTRY DOOR SLIDE IS DIFFICULT TO ENGAGE AND DISENGAGE / [01] REPOSITIONED FWD ENTRY DOOR SLIDE GIRT BAR FLAP IAW AMM 25-66-01.SDR SWAA2022081742699Girt Bar · out of positionFA REPORTS FRONT SERVICE DOOR ESCAPE SLIDE GURT BAR IS DIFFICULT TO PULL OUT OF THE HOOKS IN THE UNARMED (STORED) POSTION / [01] ADJUSTED GURT BAR CLIPS. OPS CKS GOOD PER MM 25-66-01SDR SWAA2022081642357Slide · pulledPROVISIONING OPENED FORWARD SERVICE DOOR AND GURT BAR CAUGHT EDGE OF DOOR FRAME AND PARTIALLY PULLED ESCAPE SLIDE COVER OPEN. SLIDE DID NOT INFLATE. / [01] REPACKED FORWARD SERVICE DOOR SLIDE PER MM 25-66-01-400-804.SDR SWAA2022032083234Light · inoperativeFOWARD SERVICE DOOR SLIDE LIGHT IS INOP / [01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD SERVICE DOOR SLIDE LIGHT PER AMM 33-51-04-960-801;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2022032080212Light · inoperativeL/H OVERWING ESCAPE GROUND ILLUMINATION LIGHT IS INOP L547 / [01] RELAMPED L/H OVERWING ESCAPE GROUND ILLUMINATION LIGHT L547 AND PERFORMED A GOOD INSTALLATION TEST PER AMM 33-51-04-960-801;[02] VERIFIED CORRECTIVE ACTION 1. TEST GOOD.SDR SWAA2022032080213Light · inoperativeBOTH L/H AND R/H OVERWING ESCAPE HATCH LIGHT ASSEMBLIES ARE INOP (L751) / [01] REPLACED LAMPS FOR L/H AND R/H OVERWING ESCAPE HATCH EMERGENCY EXIT LIGHTS AND PERFORMED GOOD TEST PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2022032080214Battery Pack · inoperativeALL EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP / [01] REPLACED BATTERY PACK M1673 AND PERFORMED GOOD TEST PER AMM 33-51-00-960-805.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2022032176447Scuff Plate · crackedAFT CARGO BAY FWD SCUFF PLATE IS CRACKED / [01] WELDED CRACK ON RADIUS OF ACB; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT# 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL ID; E10583. S/N; KJ256554;[02] VERIFIED FWD CORNER SCUFSDR SWAA2022032175520Gusset · crackedFWD CARGO BAY GUSSET CRACKED BS 500D STR 19L/H / [01] REMOVED FWD CARGO BAY GUSSET AT BS 500D; STR 19 L/H IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW GUSSET PART# 143A9481-5; LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 174; REV:-; OK TO INSTALLSDR SWAA2022032175521Gusset · crackedFWD CARGO BAY GUSSET CRACKED BS 500D STR 19R/H / [01] REMOVED FWD CARGO BAY GUSSET AT BS 500D; STR 19 R/H IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW GUSSET PART#143A9481-6; LOCATED AND DRILL IAW SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 174; REV:-; OK TO INSTALL;[0SDR SWAA2022032174003Intercostal · crackedAFT CARGO BAY INTERCOSTAL CRACKED BS 946 LBL 25 WL 163 / [01] REMOVED INTERCOSTAL AT ACB AT BS 927 TO 947 RBL 25 WL 163 AND EVALUATED DAMAGE ON INTERCOSTAL NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM; WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-40-02 AND 51-10-02 SDR SWAA2022032173452Angle · corrodedCORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE IN ACB BS 947 RBL 22.5; WL 179.8 / [01] REMOVED BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS 947 ;RBL 22.5 ; WL 179.8 AND EVALUATED DAMAGE BULKHEAD SUPPORT ANGLE NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM; SDR SWAA2022032171162Angle · crackedRT HORIZONTAL STABILIZER RIB 4 (STAB STA 120.30) HAS CRACK AT FWD ATTACH ANGLE / [01] VERIFIED APPLICABILITY.<BR>REMOVED DAMAGED FWD ATTACH ANGLE AT RT HORIZONTAL STABILIZER RIB 4. IAW B737 SRM 51-40-02.;[02] EDITED REPAIR TYPE IN MEASUREMENT FIELD. ATTACH ANGSDR SWAA2022032170784Rib · crackedRT HORIZONTAL STABILIZER RIB 4 (STAB STA120.30) HAS CRACK AT STIFFENER #4 LOWER RADIUS / [01] VERIFIED APPLICABILITY OF REPAIR MANUAL SRM 55-10-09-2R-5.<BR>REMOVED DAMAGED AT RT HORIZONTAL STABILIZER RIB 4 (STAB STA120.30) STIFFENER #4 LOWER RADIUS. IAW B737 SSDR SWAA2022032169450Floorboard · out of toleranceFAB NEW 232HF FLOOR BOARD / [01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIG 3 SECTION 43 .<BR>FLOOR PANEL 232HF BEYOND ECONOMICAL REPAIR PER SRM 53-00-50-1A-1 PARA 4 A-E . REPLACE FLOOR PANEL AS GIVEN IN SRM 53-00-50-2R-0 PARA 1 A NOTE.;[02] USING MATESDR SWAA2022032168800Rail · corrodedACB FLOOR RAIL RBL3. HAS VISIBLE TWIST BETWEEN BS767 AND BS787 / [01] SRM 53-00-53-1A-2 ALLOWABLE DAMAGE IS APPLICABLE FOR THIS AIRCRAFT.;[02] DAMAGE TO RAIL FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2.;[03] REMOVED DAMAGED PART OF RAIL IASDR SWAA2022032168798Rail · corrodedACB FLOOR RAIL CORRODED AT BS767+5'; RBL3 / [01] REMOVED CORROSION ON ACB FLOOR RAIL AT BS 767+5 RBL 3 IN AREA OF L=1' X W=3' D=.008' REMAINING THICKNESS =.055' FROM ORIGINAL THICKNESS .063' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-01-2; SRM 53-00-53-1A-2 B SDR SWAA2022032169067Shield · corrodedCORROSION ON AFT SHIELD AT AFT CARGO BAY BS847+8 RBL22. / [01] CORROSION ON SHIELD IS OUT OF LIMITS DUE TO NO ARE GIVEN SRM AT ACB BS 847+8' RBL 22 WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR. 9.;[02] RECEIVED NEW SHIELD P/N 146A8127Y10ATSMRO ; LOT: 1SDR SWAA2022032169069Splice · corrodedCORROSION ON FLOOR SUPPORT SPLICE AROUND FASTENER HOLES AT AFT CARGO BAY BS887 BL0 / [01] ACB FLOOR SPLICE BS887; FOUND THERE ARE NO ALLOWABLE DAMAGE LIMITS PER SRM. REPAIR BY REPLACEMENT OF PART;[02] EDITED DAMAGE CHART;[03] REMOVED ACB FLOOR SPLICE AT BS887 SDR SWAA2022032169071Track · corrodedCORROSION ON TRACK AT AFT CARGO BAY BS887+2; BS927+8 RBL13. / [01] REMOVED CORROSION ON TRACK AT AFT CARGO BAY BS 887+2; RBL 13; WORK AREA L 1.0'X W 1.0'X D 0.024'; BS 927+8; RBL 13; WORK AREA L 1.0'X W 1.0'X D 0.021 ; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-5SDR SWAA2022032169073Angle · corrodedCORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS947 LBL9 TO RBL13. / [01] REMOVED CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS 947 LBL9 TO RBL13 IAW SRM 51-10-HOLE NOT DRILLED AND SEVERAL HOLES NOT COUNTERSUNK. SEE SSDR SWAA2022032169077None · corrodedCORROSION ON STRINGER CLIP AT AREA AFT OF ACB BS987 S-22L. MARKED. / [01] EVALUATED STRINGER CLIP AT AREA AFT OF ACB BS987 S-22L. AND NOT FOUND ALLOWABLE DAMAGE LIMITS ; MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED STRINGER CLIP AT AREA AFT OF ACSDR SWAA2022032169076Web · corrodedCORROSION ON WEB AT AFT CARGO BAY BS866 S-18R. MARKED. / [01] REMOVED CORROSION ON WEB AT AFT CARGO BAY BS 866 S-18R IAW SRM 51-10-02 PARAGRAPH 15 ;EVALUATED DAMAGE ;REWORKED AREA ;THE DEPPEST AREA BS 866 STR 18R; DIMENSION L=3' ;W=2' DEPTH=0.012' ORIGINAL THISDR SWAA2022032168809Intercostal · corrodedLOWER DOOR SURROUND STUCTURE INTERCOSTAL CORROSION LOWER SURFACE COMMON TO NUT PLATES. RBL19.5; BS807-3'; BS807+2'; BS807+5.75'; BS807+9.5'; BS807+13'; BS807+16.75'; BS827+4'; BS827+7.5'; BS827+11.25' / [01] SRM 53-60-15-1A-1 IS FOUND TO BE APPLICABLE;[02] REMSDR SWAA2022032168780Track · crackedACB TRACK CRACKED IN RADIUS; BS767; RBL13.84 / [01] ACB TRACK IN RADIUS AT BS 767;RBL 13.84 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;[10] INSTALLED NEW CARGO TRACK BTW B/S 747+10' TO B/S 887 RBL 13.84 ; IAW SRM 51-40-02 AND DWG 146A7500 REV:A;[11] VERIFSDR SWAA2022032169065Stiffener · crackedCRACKED STIFFENER BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS918 RBL10. / [01] REMOVED STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS918 RBL10 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW STIFFENER AT ACB BS918 RBL10 IAW SRM 51-40-05 AND BOEING DWG 147A722SDR SWAA2022032169072Stiffener · crackedCRACKED STIFFENER BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS914 RBL10. / [01] REMOVED STIFFENER BEHIND WATER SERVICE PANEL ACB BS 914 RBL10 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW STIFFENER AT ACB BS914 RBL 10 IAW SRM 51-40-05 AND BOEING DWG 147A7221SDR SWAA2022032168772Support · corrodedCORROSION ON FCB L/H FLOOR TO SIDEWALL SUPPORT FROM STA 400+1 TO STA 500B+18; LBL 24; WL 156. / [01] BLENDED ALL CORROSION FROM STA 400+1 TO STA 500B+18 LBL24 IAW SRM 51-10-02-0G-0G<BR><BR>STA 400+6' : 0.002' <BR>STA 400+10' : 0.003'<BR>STA 400+18' : 0.002'<BRSDR SWAA2022032168773Support · corrodedCORROSION ON FCB AFT BULKHEAD SUPPORT FROM RBL 24 TO LBL 24; STA 500D; WL 156. / [01] NO ALLOWABLE DAMAGE LIMITS FOR FCB AFT BULKHEAD CTR SUPPORT ANGLE PER SRM. REPAIR BY REPLACEMENT OF PART;[02] REMOVED FCB AFT BULKHEAD CTR SUPPORT ANGLE PER SRM 51-40-02;[03]SDR SWAA2022032168775Shield · corrodedCORROSION ON FCB DOOR CUT-OUT FWD SHIELD FROM STA 420 TO 440; RBL 24; WL 156. / [01] NO ENTRIES FOR ALLOWABLE DAMAGE ON SRM FOR THIS ITEM; REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; PAR. 9.;[02] LOCATED AND DRILLED NEW FCB DOOR CUT-OUT FWD. SHIELD BS420 - BSSDR SWAA2022032168768Support · corrodedCORROSION ON FCB R/H FLOOR TO SIDEWALL SUPPORT FROM STA 500A TO STA 500D; RBL 24; WL 156. / [01] SRM 3-00-53-1A-2 IS APPLICABLE<BR><BR>REMOVED CORROSION FROM 16EA. LOCATIONS AT FCB R/H FLOOR TO SIDEWALL SUPPORT FROM STA 500A TO STA 500D; RBL 24; WL 156. IAW SRSDR SWAA2022032168769Shield · corrodedCORROSION ON FCB DOOR CUT-OUT AFT SHIELD FROM STA 480+14 TO STA 500A; RBL 24; WL 156. / [01] NO ENTRIES FOR ALLOWABLE DAMAGE ON SRM FOR THIS ITEM; REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; PAR. 9;[02] LOCATED AND DRILLED NEW FCB CUT-OUT DOOR AFT SHIELD FROMSDR SWAA2022032168774Web · corrodedCORROSION ON FCB DOOR CUT-OUT SUB-THRESHOLD WEB FROM STA 460 TO STA 480+4; RBL 28; WL 156. / [01] REMOVED CORROSION ON FCB DOOR CUT-OUT SUB-THRESHOLD WEB AT AREA 1 BS460 RBL 28 L=1' X W=1' D= 0.009' REMAINING THICKNESS = 0.036 FROM ORIGINAL THICKNESS= 0.45'. ASDR SWAA2022032168791Intercostal · corrodedACB INTERCOSTAL AT BS767-BS787 CORRODED TOP AND I/B SURFACES. RBL20; BS767+4.5' TO 7'; BS767+18' / [01] REMOVED CORROSION FROM ACB INTERCOSTAL AT BS767-787 RBL20 MEASURED 3.3'L X 1.9'W AND 0.007' DEEP; ORIGINAL THICKNESS OF 0.063' FOUND OUT OF LIMITS PER SRM 5SDR SWAA2022032168782Angle · corrodedACB LOWER DOOR SURROUND STRUCTURE; ANGLE COMMON TO FWD SHIELD AND INTERCOSTAL CORRODED. BS787+1.25' TO BS787+2.25'; RBL20.5; WL157 / [01] REMOVED CORROSION ACB LOWER DOOR SURROUND STRUCTURE ;ANGLE COMMON BS 787+1.25' TO BS 787+2.25' RBL 20.05 WL 157;DIMENSION SDR SWAA2022032185761Intercostal · corrodedACB LOWER DOOR SURROUND STRUCTURE; ANGLE COMMON TO FWD SHIELD AND INTERCOSTAL CORRODED. BS787+1.25' TO BS787+2.25'; RBL20.5; WL157 / [01] REMOVED CORROSION ACB LOWER DOOR SURROUND STRUCTURE ;ANGLE COMMON BS 787+1.25' TO BS 787+2.25' RBL 20.05 WL 157;DIMENSION SDR SWAA2022032168785Support · corrodedACB RH FLOOR TO SIDEWALL SUPPORT CORRODED. RBL21; BS747; BS747+5.5'; BS747+8.5'; BS747+10.5'; BS747+14.5'; BS747+15'; BS747+18.5'; BS767. / [01] REMOVED CORROSION ON ACB RH FLOOR TO SIDEWALL SUPPORT RBL 21 ; WORK AREAS BS 747; L 1.0'X W 1.0'; D 0.014'; BS 747+
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